RU2138422C1 - Устройство для гашения вращающего момента, предназначенное для вертолета - Google Patents

Устройство для гашения вращающего момента, предназначенное для вертолета Download PDF

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Publication number
RU2138422C1
RU2138422C1 RU95107156A RU95107156A RU2138422C1 RU 2138422 C1 RU2138422 C1 RU 2138422C1 RU 95107156 A RU95107156 A RU 95107156A RU 95107156 A RU95107156 A RU 95107156A RU 2138422 C1 RU2138422 C1 RU 2138422C1
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Russia
Prior art keywords
blades
channel
screw
air flow
tail
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RU95107156A
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English (en)
Russian (ru)
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RU95107156A (ru
Inventor
Ришар Марз Анри-Жам
Жан Люк Рутьо Венсан
Луи Арно Жий
Элиан Арно Реми
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Эрокоптер Франс
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Application filed by Эрокоптер Франс filed Critical Эрокоптер Франс
Publication of RU95107156A publication Critical patent/RU95107156A/ru
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8254—Shrouded tail rotors, e.g. "Fenestron" fans

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
RU95107156A 1994-05-04 1995-05-03 Устройство для гашения вращающего момента, предназначенное для вертолета RU2138422C1 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9405477 1994-05-04
FR9405477A FR2719549B1 (fr) 1994-05-04 1994-05-04 Dispositif anti-couple à rotor caréné et modulation de phase des pales, pour hélicoptère.

Publications (2)

Publication Number Publication Date
RU95107156A RU95107156A (ru) 1997-02-20
RU2138422C1 true RU2138422C1 (ru) 1999-09-27

Family

ID=9462870

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95107156A RU2138422C1 (ru) 1994-05-04 1995-05-03 Устройство для гашения вращающего момента, предназначенное для вертолета

Country Status (8)

Country Link
US (1) US5566907A (fr)
EP (1) EP0680871B1 (fr)
JP (1) JP3043592B2 (fr)
CN (1) CN1061618C (fr)
CA (1) CA2148420C (fr)
DE (1) DE69501847T2 (fr)
FR (1) FR2719549B1 (fr)
RU (1) RU2138422C1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2538497C1 (ru) * 2013-12-03 2015-01-10 Открытое акционерное общество "Камов" Рулевой винт вертолета, установленный в туннеле
RU2557683C2 (ru) * 2013-10-18 2015-07-27 Эйрбас Хеликоптерс Дойчланд Гмбх Вертолет с поперечным каналом
RU2766641C2 (ru) * 2017-12-22 2022-03-15 ЛЕОНАРДО С.п.А. Вертолет с системой противовращения

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WO1998036966A1 (fr) * 1997-02-21 1998-08-27 California Institute Of Technology Rotors a pales desaccordees
JP3051357B2 (ja) * 1997-03-26 2000-06-12 株式会社コミュータヘリコプタ先進技術研究所 主ロータトルク補正装置
US6416015B1 (en) 2001-05-01 2002-07-09 Franklin D. Carson Anti-torque and yaw-control system for a rotary-wing aircraft
US7058556B2 (en) * 2001-09-26 2006-06-06 Goodrich Pump & Engine Control Systems, Inc. Adaptive aero-thermodynamic engine model
US6755374B1 (en) 2003-01-27 2004-06-29 Franklin D. Carson Anti-Torque and yaw-control system for a rotary-wing aircraft
JP2008506582A (ja) * 2004-07-16 2008-03-06 ベル ヘリコプター テクストロン インコーポレイテッド ヘリコプタ用逆トルク装置
FR2926786B1 (fr) 2008-01-30 2010-02-19 Eurocopter France Procede d'optimisation d'un rotor anti-couple carene a gene acoustique minimale pour un giravion, notamment un helicoptere, et rotor anti-couple carene ainsi obtenu
EP2123557B1 (fr) * 2008-05-22 2011-04-27 Agusta S.p.A. Pale de rotor anticouple
DE102008057715B4 (de) 2008-11-17 2020-09-24 Liebherr-Aerospace Lindenberg Gmbh Heckrotorsystem
DE102008058029B3 (de) * 2008-11-18 2010-01-07 Deutsches Zentrum für Luft- und Raumfahrt e.V. Hubschrauber
CN102712364B (zh) * 2009-05-22 2015-08-19 贝尔直升机泰克斯特龙公司 用于减弱振动的旋翼桨叶间距
GB2482545B (en) * 2010-08-06 2017-05-03 Ge Aviat Systems Ltd Aircraft propellers with composite blades mounted to a single propeller hub
FR2968272B1 (fr) * 2010-12-06 2013-07-12 Eurocopter France Element de structure ameliore d'un giravion pour diminuer la trainee aerodynamique.
FR2969120B1 (fr) * 2010-12-15 2013-08-30 Eurocopter France Pale amelioree pour dispositif anti-couple d'helicoptere
FR2987031B1 (fr) 2012-02-21 2014-10-24 Eurocopter France Aeronef a voilure muni d'un rotor arriere, et procede pour optimiser le fonctionnement d'un rotor arriere
FR2987346B1 (fr) 2012-02-27 2014-08-29 Eurocopter France Pale de rotor, rotor, aeronef, et procede
EP2671798B1 (fr) * 2012-06-08 2015-08-05 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Hélicoptère avec un conduit transversal
EP2706009B1 (fr) 2012-09-07 2016-04-27 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Empennage d'un hélicoptère
EP2799334B1 (fr) 2013-04-29 2016-09-07 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Ensemble rotatif de pale à aileron toroïde extérieur aérodynamique pour un ensemble rotatif de propulsion carénée
CN103438024A (zh) * 2013-07-03 2013-12-11 浙江理工大学 一种叶片非均匀分布的小型轴流风扇
FR3014838B1 (fr) * 2013-12-17 2015-12-25 Eurocopter France Giravion equipe d'un rotor arriere anti couple participant selectivement a la sustentation et a la propulsion en translation du giravion
EP2913270B1 (fr) 2014-02-28 2016-02-24 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Giravion avec au moins un rotor principal et au moins un rotor anti-couple
EP2913271A1 (fr) 2014-02-28 2015-09-02 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Giravion avec au moins un rotor principal et au moins un rotor anti-couple
EP2913269B1 (fr) 2014-02-28 2019-01-16 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Giravion avec au moins un rotor principal et au moins un rotor anti-couple
CN104014983B (zh) * 2014-05-29 2016-08-31 哈尔滨工业大学（威海） 一种导管螺旋桨加工方法
EP3225537B1 (fr) * 2016-04-01 2019-07-24 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Hélicoptère avec un fuselage et une poutre de queue composite
EP3366584B1 (fr) 2017-02-27 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Dispositif de commande de pas pour un fenestron d'un giravion
CN107089322A (zh) * 2017-04-26 2017-08-25 浙江点辰航空科技有限公司 一种变升力结构油动多旋翼无人机
EP3424818B1 (fr) 2017-07-06 2020-12-30 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Moyeu de rotor pour un fenestron d'un giravion
EP3424817B1 (fr) 2017-07-06 2020-09-02 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Moyeu de rotor pour rotor arrière d'un giravion
US10822101B2 (en) * 2017-07-21 2020-11-03 General Electric Company Vertical takeoff and landing aircraft having a forward thrust propulsor
EP3434590B1 (fr) 2017-07-27 2019-11-27 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Élément de transfert de commande pour un dispositif de commande de pas du fenestron d'un giravion
US10946953B2 (en) * 2017-12-20 2021-03-16 Wing Aviation Llc Multi-rotor tonal noise control for UAV
JP7149498B2 (ja) * 2018-07-26 2022-10-07 パナソニックＩｐマネジメント株式会社 無人飛行体、情報処理方法およびプログラム
US10889366B2 (en) * 2018-09-21 2021-01-12 Textron Innovations Inc. Ducted thrusters
FR3087832B1 (fr) 2018-10-26 2020-10-16 Airbus Helicopters Systeme carene et aeronef
CN110750836A (zh) * 2019-10-15 2020-02-04 北京电子工程总体研究所 一种基于稳态锥动的飞行器俯仰阻尼力矩计算方法
US11203421B1 (en) * 2020-06-19 2021-12-21 Textron Innovations Inc. Passive tip gap management systems for ducted aircraft
US11479350B2 (en) 2020-06-19 2022-10-25 Textron Innovations Inc. Tip gap monitoring systems for ducted aircraft
US11407504B2 (en) 2020-06-19 2022-08-09 Textron Innovations Inc. Tip gap control systems with inner duct control surfaces
US11370536B2 (en) 2020-06-19 2022-06-28 Textron Innovations Inc. Tip gap control systems with active blade tips
CN113928554B (zh) * 2021-11-19 2023-04-28 中国直升机设计研究所 一种直升机尾部反扭矩装置及气动设计方法

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FR1531536A (fr) * 1967-05-22 1968-07-05 Sud Aviation Hélice ou rotor à pas variable
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FR2534222A1 (fr) * 1982-10-06 1984-04-13 Aerospatiale Agencement de rotor de queue a poussee accrue pour aeronef a voilure tournante et dispositif pour accroitre la poussee d'un tel agencement
FR2542695B1 (fr) * 1983-03-18 1985-07-26 Aerospatiale Helice multipale a pas variable a pale s en materiaux composites demontables individuellement, procede de fabrication de telles pales et pales ainsi realisees
DE3605086A1 (de) * 1986-02-18 1987-08-27 Rhein Flugzeugbau Gmbh Ausbildung von im zustrom zu luftschrauben, mantelschrauben und/oder fans liegenden bauteilen zur verringerung des von ihnen verursachten zusatzlaerms sowie zur verringerung der wechselbelastung der propellergeblaese
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Книга "Авиационная акустика". Ч. 1. - М.: Машиностроение, 1986, с. 138-140. *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2557683C2 (ru) * 2013-10-18 2015-07-27 Эйрбас Хеликоптерс Дойчланд Гмбх Вертолет с поперечным каналом
RU2538497C1 (ru) * 2013-12-03 2015-01-10 Открытое акционерное общество "Камов" Рулевой винт вертолета, установленный в туннеле
RU2766641C2 (ru) * 2017-12-22 2022-03-15 ЛЕОНАРДО С.п.А. Вертолет с системой противовращения

Also Published As

Publication number Publication date
DE69501847T2 (de) 1998-11-26
JPH08133190A (ja) 1996-05-28
CA2148420C (fr) 2003-01-07
JP3043592B2 (ja) 2000-05-22
EP0680871A1 (fr) 1995-11-08
FR2719549A1 (fr) 1995-11-10
RU95107156A (ru) 1997-02-20
DE69501847D1 (de) 1998-04-30
FR2719549B1 (fr) 1996-07-26
EP0680871B1 (fr) 1998-03-25
CA2148420A1 (fr) 1995-11-05
CN1061618C (zh) 2001-02-07
US5566907A (en) 1996-10-22
CN1121020A (zh) 1996-04-24

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